DHC-8 Dash 8 vs L-29 Delfin
Overview
The DHC-8 Dash 8 and the L-29 Delfin are both Military Training Aircraft, manufactured by De Havilland Canada and Aero respectively.
Top speed is 451 km/h for the DHC-8 Dash 8 vs 655 km/h for the L-29 Delfin. The DHC-8 Dash 8 has an operational range of 1,600 km vs 894 km for the L-29 Delfin. The L-29 Delfin operates at altitudes up to 11,500 m compared to 9,144 m for the DHC-8 Dash 8. At 15,649 kg MTOW, the DHC-8 Dash 8 is 4.4x the L-29 Delfin's 3,540 kg.
The DHC-8 Dash 8 has been produced in 1,258 units vs 3,665 for the L-29 Delfin. Unit cost is $27M for the DHC-8 Dash 8 vs $0.2M for the L-29 Delfin. The L-29 Delfin first flew 24 years before the DHC-8 Dash 8 (1959 vs 1983).
| Canadian turboprop-powered regional airliner, widely adopted globally for short-haul commuter flights throughout the late 20th century. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Training Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 20 June 1983 |
| Year introduced | 1984 |
| Number produced | 1258 units |
| Average unit price | $27 million |
| Czechoslovakian jet trainer, utilized extensively during the Cold War, and exported broadly to Warsaw Pact and other nations. | |
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| Origin country | 🇨🇿 Czechia |
| Category | Military Training Aircraft |
| Manufacturer | Aero |
| First flight | 5 April 1959 |
| Year introduced | 1961 |
| Number produced | 3665 units |
| Average unit price | $200K |
| Wing area | 54.4 m² ◉ |
| Wingspan | 26.0 m â—‰ |
| Height | 7.5 m â—‰ |
| Length | 22.0 m â—‰ |
| Maximum speed | 451 km/h â—‰ |
| Operational range | 1,600 km â—‰ |
| Service ceiling | 9,144 m â—‰ |
| Max. takeoff weight | 15,649 kg â—‰ |
| Empty weight | 14,787 kg â—‰ |
| Total thrust | 2 x 671 kW â—‰ |
| Wing area | 20.0 m² ◉ |
| Wingspan | 10.3 m â—‰ |
| Height | 3.1 m â—‰ |
| Length | 10.8 m â—‰ |
| Maximum speed | 655 km/h â—‰ |
| Operational range | 894 km â—‰ |
| Service ceiling | 11,500 m â—‰ |
| Max. takeoff weight | 3,540 kg â—‰ |
| Empty weight | 2,280 kg â—‰ |
| Total thrust | 1 x 890 kgf â—‰ |
Performance Radar Chart
Detailed Comparison
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